Modification of the properties of aircraft engine compressor blades by uninterrupted and pulsed-ion beams
| Parent link: | Surface and Coatings Technology: Scientific Journal Vol. 96, iss. 1.— 1997.— [P. 39-44] |
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| Other Authors: | , , , |
| Summary: | Title screen The influence of uninterrupted and arc-pulsed ion implantation, high-power ion beam treatment and final annealing regimes on the chemical composition and phase-structural state of surface layers and on the surface properties of gas turbine engine compressor blades manufactured from refractory alloys was investigated. Long-term full-scale tests of the production and irradiated compressor blades were carried out under gas turbine engine operating conditions. After completion of the tests the physical-chemical state of the blades was studied. Режим доступа: по договору с организацией-держателем ресурса |
| Language: | English |
| Published: |
1997
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| Subjects: | |
| Online Access: | http://dx.doi.org/10.1016/S0257-8972(97)00170-9 |
| Format: | Electronic Book Chapter |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=645333 |
| Summary: | Title screen The influence of uninterrupted and arc-pulsed ion implantation, high-power ion beam treatment and final annealing regimes on the chemical composition and phase-structural state of surface layers and on the surface properties of gas turbine engine compressor blades manufactured from refractory alloys was investigated. Long-term full-scale tests of the production and irradiated compressor blades were carried out under gas turbine engine operating conditions. After completion of the tests the physical-chemical state of the blades was studied. Режим доступа: по договору с организацией-держателем ресурса |
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| DOI: | 10.1016/S0257-8972(97)00170-9 |